Aerospace Engineering
GATE AE purpose:exam-prep PYQs
Build your understanding with focused practice from past exam papers.
Questions 291–300 of 650. Imported answers require independent review unless marked reviewed.
Question 31
Open questionAENAT1 markNeeds review
The arc length of the parametric curve:
from
to
is equal to ______ (round off to one decimal place).Log in to check the answer
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An unpowered glider is flying at a glide angle of 10 degrees. Its lift-to-drag ratio is ______________ (round off to two decimal places).
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The two-dimensional plane-stress state at a point is:
The normal stress,
, on a plane inclined 45° as shown in the figure is ___
(round off to the nearest integer). 
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In a static test, a turbofan engine with bypass ratio of 9 has core hot exhaust speed 1.5 times that of fan exhaust speed. The engine is operated at a fuel to air ratio of
. Both the fan and the core streams have no pressure thrust. The ratio of fan thrust to thrust from the core engine is _____ (round off to one decimal place).Log in to check the answer
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In a single stage turbine, the hot gases come out of stator/ nozzle at a speed of 500 m/s and at an angle of 70 degrees with the turbine axis as shown. The design speed of the rotor blade is 250 m/s at the mean blade radius. The rotor blade angle,
, at the leading edge is ________ degrees (round off to one decimal place). 
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Open questionAEMCQ2 marksNeeds review
The height of a right circular cone of maximum volume that can be enclosed within a hollow sphere of radius
isYour answerChoose one option.
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Consider the differential equation
. The boundary conditions are
and
at
. Then the value of
at
isYour answerChoose one option.
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Open questionAEMCQ2 marksNeeds review
Consider the partial differential equation
where
are real. If
, where
and
are real functions, which one of the following statements can be true?Your answerChoose one option.
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A cylindrical object of diameter 900 mm is designed to move axially in air at 60 m/s. Its drag is estimated on a geometrically half-scaled model in water, assuming flow similarity. Coefficients of dynamic viscosity and densities for air and water are
Pa-s, 1.2 kg/m
and
Pa-s, 1000 kg/m
respectively. Drag measured for the model is 220 N. Drag experienced by the full-scale object is ____ N (round off to the nearest integer).Your answerChoose one option.
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Open questionAEMCQ2 marksNeeds review
Consider a conventional subsonic fixed-wing airplane.
is the Oswald efficiency factor and
is the aspect ratio. Corresponding to the minimum
, which of the following relations is true?Your answerChoose one option.
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